Fiber optic manufacturing in space
Abstract
Aspects of the embodiments are directed to systems and methods for forming an optical fiber in a low gravity environment, and an optical fiber formed in a low gravity environment. The system can include a preform holder configured to secure a preform; a heating element secured to a heating element stage and residing adjacent the preform holder; a heating element stage motor configured to move the heating element stage; a tension sensor; a spool; a spool tension motor coupled to the spool and configured to rotate the spool; and a control system communicably coupled to the heating element stage motor and the spool tension motor and configured to control the movement of the heating element stage based on a rotational speed of the spool. The optical fiber can include a fluoride composition, such ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN), and can be characterized by an insertion loss in a range from 13 dB/1000 km to 120 dB/1000 km.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1. A system for forming an optical fiber in a low gravity environment, the system comprising:
a preform holder configured to secure a preform;
a heating element secured to a heating element stage and residing adjacent the preform holder;
a heating element stage motor configured to move the heating element stage;
a tension sensor;
a spool;
a spool tension motor coupled to the spool and configured to rotate the spool; and
a control system communicably coupled to the heating element stage motor and the spool tension motor and configured to control the movement of the heating element stage based on a rotational speed of the spool.
2. The system of claim 1 , further comprising a preform secured in the preform holder, wherein the tension sensor is coupled to the preform holder and configured to monitor a tension on the preform.
3. The system of claim 2 , wherein the heating element surrounds the preform.
4. The system of claim 1 , further comprising a spool translation motor configured to translate the spool along a long axis of the spool.
5. The system of claim 1 , wherein the control system is configured to control a temperature of the heating element.
6. The system of claim 1 , wherein the control system is configured to control the spool tension motor to control a tension applied to a preform.
7. The system of claim 1 , wherein the tension sensor comprises a load cell.
8. The system of claim 1 , further comprising a surface coating retention element surrounded by the heating element, the surface coating retention element configured to apply a coating onto a fiber.
9. A method for forming an optical fiber in a low gravity environment, the method comprising:
providing a preform in a preform drawing apparatus in the low gravity environment;
engaging the preform with a spool under an initial temperature;
turning the spool until a desired tension on the preform has been reached;
increasing the temperature of the preform until a desired spool speed is reached; and
locking the temperature of the preform.
10. The method of claim 9 , further comprising:
heating a coating material with the preform; and
coating the optical fiber with the coating material during formation of the optical fiber.
11. The method of claim 9 , wherein increasing the temperature of the preform comprises heating the preform in an oven that surrounds the preform.
12. The method of claim 11 , further comprising adjusting a position of the oven as the preform changes, wherein adjusting the position of the oven is based, at least in part, on the spool speed.
13. The method of claim 9 , further comprising heating the preform to an initial temperature prior to engaging the preform with the spool.
14. The method of claim 9 , wherein the desired spool speed is based, at least in part, on a desired diameter of the optical fiber.
15. The method of claim 9 , wherein turning the spool comprises applying a torque to the spool by a computer-controlled motor.
16. The method of claim 9 , wherein providing the preform in a preform drawing apparatus in the low gravity environment comprises providing the preform in a platform or vehicle orbiting the Earth.
17. An optical fiber drawn in a low gravity environment in accordance with the method of any of claims 9 - 16 .
18. The optical fiber of claim 17 , wherein the optical fiber comprises fluoride.
19. The optical fiber of claim 18 , wherein the optical fiber comprises ZrF4-BaF2-LaF3-AlF3-NaF (ZBLAN).
20. The optical fiber of claim 17 , wherein the optical fiber comprises an insertion loss in a range from 13 dB per 1000 km to 120 dB per 1000 km.Cited by (0)
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